V18 冷加工工艺 标准查询与下载

NF L17-305:2012 航空航天系列 涂料和清漆 军用非铬系列非腐蚀抑制双组分冷硬化底漆

Aerospace series - Paints and varnishes - Chromate free non corrosion inhibiting two components cold curing primer for military application.

SAE AMS2430S-2012 自动化喷丸加工

This specification covers the requirements for automatic shot peening of surfaces of parts by impingement of media, including metallic, glass or ceramic shot.

Shot Peening, Automatic

SAE AMS-P-81728A-2012 锡铅镀层(电解沉积)

This specification covers the requirements for electrodeposited tin-lead plating intended for use as a coating for corrosion protection and as a base for soldering.

Plating, Tin-Lead (Electrodeposited)

NF L10-303:2012 航空航天系列.镉真空镀

Aerospace series - Vacuum deposition of cadmium.

SAE AMS2447D-2012 热喷雾高速氧化/燃烧过程镀涂

This specification covers the requirements for thermal spray coatings applied using the high velocity oxygen fuel (HVOF) combustion process. This specification is not intended to be used for duples coatings, i.e., the application of the coating over a previously applied coating. This process has been used typically to provide coatings of lower porosity and higher adhesive, and/or cohesive, strength than generally attainable with typical plasma spray processes for applications requiring wear, heat, and corrosion resistance and for dimensional restoration, but usage is not limited to such applications.

Coating, Thermal Spray High Velocity Oxygen/Fuel Process

SAE AMS2431/5B-2011 表面硬化钢喷丸的介质

The complete requirements for procuring the product shall consist of this document and the latest issue of the basic specification AMS 2431.

Peening Media, Case Hardened Steel Peening Balls

SAE AMS2429D-2011 电镀,青铜氮化电镀法90Cu 10Sn

This specification covers the requirements for electrodeposited bronze plate and subsequent removal. This process has been used typically as a maskant to prevent nitriding of surfaces on which nitriding is neither required nor permitted, but usage is not limited to such applications.

Plating, Bronze Nitriding Stop-off 90Cu 10Sn

SAE AMS2434D-2011 锡锌合金电镀

This specification covers the requirements for the electrodeposition of tin-zinc plating on metal parts and the properties of the deposit. This plating has been used typically as a corrosion resistant plating where cadmium cannot be used, as a replacement for tin plating where tin whisker growth is a concern, a coating for fasteners where thread lubricity is desirable, and for parts which are to be joined using tin-lead solders, but usage is not limited to such applications.

Plating, Tin-Zinc Alloy

SAE AMS2451C-2011 刷镀一般要求

This specification and its supplementary detail specifications establish the requirements and process controls for electrodeposition of metals by brush plating. This process has been used typically to improve surface properties such as corrosion resistance, wear resistance, and brazeability or to repair damaged, worn, or mismachined parts, but usage is not limited to such applications. This process is particularly useful for plating localized areas on-site, especially on large parts or assemblies, and for minimizing masking.

Plating, Brush General Requirements

HB/Z 20012-2011 螺栓滚压强化工艺

本指导性技术文件规定了螺栓头下圆角表面的滚压强化工艺的设备、工装、工艺过程控制、质量控制、人员和安全等要求。本指导性技术文件适用于材料强度σ≥900MPa螺栓零件的滚压强化。

Fillet rolling process of bolt

HB/Z 20001-2011 飞机钛合金整体结构件数控铣削工艺

本指导性技术文件规定了飞机钛合金整体结构件数控铣削加工的设备、工装工具、车间环境、工艺流程、工艺过程控制、质量控制、人员、安全等要求。 本指导性技术文件适用于航空企业飞机机体钛合金整体结构件以及发动机钛合金机匣、叶片的数控铣削加工。

NC milling process of titanium alloy monolithic components for aircraft

HB/Z 26-2011 航空零件喷丸强化工艺

本指导性技术文件规定了航空零件喷丸强化工艺的一般要求、工艺流程、工艺过程、质量控制与检验、喷丸后处理要求以及操作人员的培训与考核。 本指导性技术文件适用于在交变应力和应力腐蚀条件下工作的金属(如结构钢、不锈钢、祷铁、铝合金、镁合金、铜合金、钕合金、高温合金等)和铝基复合材料的零件和部件的喷丸强化。其他材料亦可参照执行。

Shot peening of aircraft parts

QJ 20037-2011 镀膜导线酸洗工艺技术要求

本标准规定了镀膜导线端头酸洗、钝化、屏蔽层接地处理工艺及其质量控制、安全防护与环境保护的技术要求。 本标准适用于航天电子产品电缆制造中ARDV辐照聚乙烯绝缘镀铜导线和KYVRP多芯辐照聚乙烯绝缘镀铜电缆的端头处理。

Technical requirements for covered wire acid pickling

QJ 2829A-2011 航天电子电气产品灌封和粘固通用技术要求

本标准规定了航天电子电气产品灌封和粘固的通用技术要求和质量要求。 本标准适用于航天电子电气产品的灌封和粘固，并可做为设计、生产、检验的依据。

General technical requirements for encapsulation and bonding of aerospace electronic products

HB/Z 20010-2011 电镀锡-铋合金工艺及质量检验

本指导性技术文件规定了铜及铜合金零件、钢铁零件电镀锡-铋合金的工艺方法及镀层质量检验等。 本指导性技术文件适用于航空产品零(组)件电镀锡-铋合金，非航空产品零(组)件可参照使用。

Process and quality inspection for Sn-Bi alloy plating

DIN EN 4476:2011 航空航天系列.涂料和清漆.冷养护中间漆;德文和英文版本EN 4476-2011

This European Standard specifies the requirements for a two component polyurethane, topcoat, with a medium degree of resistance to erosion by the effects of rain, available in a range of colours and levels of gloss, to be applied over a primer for aerospace applications on areas where rain erosion at subsonic speeds may be a problem, e. g. leading edges and air intakes. The properties specified in this standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837 Procedure A and ISO 3270 and painted with primer to EN 2435-001 and -002. The ability of the material to be used for a specific application (e. g. alternative substrate, alternative primer, specific drying conditions, etc.) should be determined by supplementary tests to confirm that the requirements of this standard are met.

Aerospace series - Paints and varnishes - Cold curing intermediate coat; German and English version EN 4476:2011

SAE AMS2452-2011 应用于硬质合金涂层的油石超精技术HVOF

This specification covers requirements for the superfinishing of High Velocity Oxygen/Fuel (HVOF) applied tungsten carbide thermal spray coatings.

Superfinishing of HVOF Applied Tungsten Carbide Coatings

SAE AMS2418H-2011 电镀铜涂层

This specification covers the requirements for electrodeposition copper. This process has been used typically to provide an anti-seize surface, to prevent carburizing of surfaces on which carburizing is neither required nor permitted, to prevent decarburization, to enhance solderability, or to provide a source of copper for furnace brazing, but usage is not limited to such applications.

Plating, Copper

SAE AMS2416L-2010 电镀和镍镉扩散

This specification covers the requirements for an electrodeposit of cadmium diffused into an electrodeposit of nickel on carbon, low-alloy, and corrosion-resistant steels. This coating has been used typically to prevent corrosion of carbon, low-alloy, and corrosion resistant steel parts that may operate in service up to 900 °F (482 °C), but usage is not limited to such applications. This process is not suitable for use on parts of complex shape where minimum nickel plate thickness requirements cannot be met and on parts whose hardness or strength would be reduced below drawing or specification requirements by heating to 640 °F (338 °C).

Plating, Nickel-Cadmium Diffused

SAE AMS2580-2010 超音速驱动的喷丸加工

This specification covers the requirements for inducing compressive residual stresses on the surface of metal parts using ultrasonically activated shot peening. Ultrasonically activated shot peening is typically used to induce compressive residual stresses on the surface layer of metallic parts to a depth up to 0.040 inch (1 mm). The shape and depth of the compressive residual stress distribution depend on the properties of the part and the ultrasonically activated shot peening process parameters. The residual stresses produced increase fatigue performance, resistance to stress-corrosion cracking, corrosion fatigue, and fretting fatigue, but its usage is not limited to such applications.

Shot Peening, Ultrasonically Activated